نتایج جستجو برای: thrust coefficient

تعداد نتایج: 178498  

2013
William R. Reed Dong-Yuan Cao Cynthia R. Long Gregory N. Kawchuk Joel G. Pickar

High velocity low amplitude spinal manipulation (HVLA-SM) is used frequently to treat musculoskeletal complaints. Little is known about the intervention's biomechanical characteristics that determine its clinical benefit. Using an animal preparation, we determined how neural activity from lumbar muscle spindles during a lumbar HVLA-SM is affected by the type of thrust control and by the thrust'...

2013
Sang-Jin Park Bum Soo Kim Dae-Lim Jee

BACKGROUND Jaw-thrust is a noxious stimulus that might induce sympathetic responses. The purpose of this study, was to evaluate the effects of jaw-thrust on sympathetic responses. METHODS We investigated seventy three patients. Patients who received general anesthesia were randomly divided into a control group (maintenance of combined airway maneuver with head tilt, open mouth by mouthpiece, ...

1992

A multiaxis thrust-vectoring nozzle designed to have equal ow-turning capability in pitch and yaw was conceived and experimentally tested for internal static performance at Langley Research Center. The cruciform-shaped, convergent-divergent nozzle turned the ow for thrust vectoring by deeecting the divergent surfaces of the nozzle, called aps. Methods for eliminating physical interference betwe...

Journal: :journal of dental research, dental clinics, dental prospects 0
tahereh jalaly farzaneh ahrari mashhad dental school foroozandeh amini

background and aims. there is no consensus about the effect of tongue thrusting on incisor position. the purpose of this study was to evaluate the position of anterior teeth in growing children with tongue thrust swallowing. materials and methods. in the present study 193 subjects with an age range of 9 to 13 years participated. all the patients were examined by a trained investigator and those...

2014
Ben de Witt

This paper investigates a slug-flow expander (SFE) for conversion of high-pressure gas/vapor into kinetic energy of liquid slugs. The energy transfer from high-pressure to kinetic energy is quantified using thrust plate measurements. Non-dimensional thrust data is used to quantify performance by normalizing measured thrust by thrust for the same water flow rate at zero air flow rate. A total of...

Journal: :Physical review 2022

A new formalism for the factorization of cross section single-hadron production in ${e}^{+}{e}^{\ensuremath{-}}$ annihilations, differential ${z}_{h}$, ${P}_{T}$, and thrust, is applied to phenomenological analysis data recently measured by BELLE Collaboration. Within this scheme ${e}^{+}{e}^{\ensuremath{-}}\ensuremath{\rightarrow}hX$ can be recast convolution a perturbatively calculable coeffi...

C. Lucas, F. Tootoonchian, Z. Nasiri-Gheidari,

In this paper a brushless permanent magnet motor is designed considering minimum thrust ripple and maximum thrust density (the ratio of the thrust to permanent magnet volumes). Particle Swarm Optimization (PSO) is used as optimization method. Finite element analysis (FEA) is carried out base on the optimized and conventional geometric dimensions of the motor. The results of the FEA deal to ...

2012
Steven Owens Malcolm Macdonald

g – standard gravitational acceleration, m/s μ gravitational constant, km/s mdry – spacecraft mass without fuel, kg mwet – spacecraft mass with total fuel, kg mhighF – high-thrust system fuel mass, kg mHSTF – hybrid system fuel mass, kg m02 – spacecraft mass after phase 1 of the transfer, kg ∆Vhigh – high-thrust only system ∆V, m/s ∆VH – high-thrust portion of hybrid system ∆V, m/s ∆VL – low-th...

ژورنال: مواد پرانرژی 2013
رضایی, محمدرضا, شیخی نارانی, مجید, صابری مقدم, علی,

Thrust chamber cooling system is an important issue in liquid missile systems. In this paper, two more applicable systems, that is, regenerative and radiation cooling systems are studied. Regenerative cooling systems, which are mostly used in high pressure thrust chambers, are normally in two forms, tubular wall structure and double wall structure. Tubular structure has mostly a square form str...

2015
Steven R. H. Barrett Christopher K. Gilmore

Previous work has characterized electrohydrodynamic (EHD) thruster performance, determining that thrust-to-power ratios are comparable with that of conventional propulsion at the laboratory scale. Achievable thrust density of EHD propulsion has yet to be experimentally quantified and could be a limiting factor in its application. In this paper, we quantify the achievable thrust density for a wi...

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